US3971023A - Parabolic reflector assembled from triangular shaped petals - Google Patents
Parabolic reflector assembled from triangular shaped petals Download PDFInfo
- Publication number
- US3971023A US3971023A US05/537,094 US53709474A US3971023A US 3971023 A US3971023 A US 3971023A US 53709474 A US53709474 A US 53709474A US 3971023 A US3971023 A US 3971023A
- Authority
- US
- United States
- Prior art keywords
- petals
- reflector
- petal
- longitudinal axis
- sub
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Images
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q15/00—Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
- H01Q15/14—Reflecting surfaces; Equivalent structures
- H01Q15/16—Reflecting surfaces; Equivalent structures curved in two dimensions, e.g. paraboloidal
- H01Q15/161—Collapsible reflectors
- H01Q15/162—Collapsible reflectors composed of a plurality of rigid panels
Definitions
- True parabolic antennae typically require substantial truss support structure and are expensive to manufacture.
- the parabolic reflector of the present invention requires no support truss and, by improving the basic design concept of the above-mentioned U.S. patent, achieves substantially parabolic shape over the entire surface of the reflector without appreciably increasing manufacturing cost, complicating field assembly or increasing shipping weight.
- One embodiment of the present invention comprises a plurality of greatly overlapping, generally triangular-shaped petals having precisely sized and positioned holes in the overlap region through which a set of fasteners are inserted to locate one petal relative to the next and to bend adjacent petals elastically to provide curvilinear transverse shape therein.
- the petals may be interlaced or alternately overlayed.
- Another embodiment of the present invention comprises a layer of generally triangular shaped petals coupled to a second fully overlapping layer of similar shaped petals, the layers being rigidly held together in substantially parabolic conformation by fasteners inserted through commonly and precisely sized and positioned holes through the petals of both layers.
- a rigid, segmented exterior rim formed to receive the outer edges of the assembled petals provides the necessary mechanical structure for mounting and positioning the reflector and for maintaining mechanical integrity over a wide range of environmental conditions.
- each petal Before assembly of either configuration reflector, each petal is essentially a flat sheet of light-weight, flexible, relatively thin, electromagnetically reflective material such as aluminum.
- the ultimate reflector configuration is determined by the precisely positioned fasteners in each petal or, alternatively in the case of the two-layer configuration wherein the inner layer petals edgewise abutt, by the shape of the abutting petal edges.
- the shape of the reflector is controlled and adjusted as desired.
- FIG. 1 is a perspective view of a microwave antenna incorporating a prior art quasi-paraboloid dish reflector.
- FIG. 2a is a top view of an eight-petal quasi-paraboloid reflector constructed according to FIG. 1 taken at the intersection of the petals with a plane perpendicular to the focal axis of that reflector prior to assembly.
- FIG. 2b is a top view of the eight-petal configuration of FIG. 2a after assembly.
- FIG. 3a is a top view of an eight-petal paraboloid reflector constructed according to one embodiment of the present invention having interlaced petals taken at the intersection of the petals with a plane perpendicular to the focal axis of that reflector prior to assembly.
- FIG. 3b is a top view of an eight-petal paraboloid reflector constructed according to one embodiment of the present invention having alternately overlayed petals taken at the intersection of the petals with a plane perpendicular to the focal axis of that reflector prior to assembly.
- FIG. 3c is a top view of the reflector configuration of FIG. 3 during assembly showing curvilinear transverse petal shape
- FIG. 4a is a side view of two cantilever beams attached to the same anchor wall.
- FIG. 4b is a side view of the top beam of FIG. 4a in bent configuration.
- FIG. 5 is a top view of a petal constructed according to one embodiment of the present invention.
- FIG. 6a is a top view of a two-layer, 16 petal paraboloid reflector constructed according to another embodiment of the present invention taken at the intersection of the petals with a plane perpendicular to the focal axis of that reflector prior to assembly.
- FIG. 6b is a top view of the reflector configuration of FIG. 6a after assembly.
- FIG. 7 is a top view of a petal constructed according to another embodiment of the present invention.
- FIG. 8 is a three-dimensional view of a parabola as it rotates about the z-axis.
- FIG. 9 is a perspective view of a rectangular plate subjected to uniform bending moments.
- each petal slightly overlapped adjacent petals for conveniently indexing the petals to one another during assembly.
- the overlap was so small that, after assembly, a small, transverse, petal-to-petal angle resulted (refer to FIGS. 1, 2a and 2b) because the overlapped portion of each petal would simply inelastically bend to the angle of the adjacent petal. No smooth, curved bending occurred along common transverse axes of the adjacent petals.
- the petals are forced to bend in the transverse direction as shown.
- the number of fasteners used at each position is essentially arbitrary taking into consideration petal material and thickness.
- the transverse direction i.e. axis
- the transverse direction is perpendicular to the longitudinal axis of the petal. If the hole positions are located accurately, the petals will form a substantially parabolic reflector. Thus the surface of a reflector need not be preformed using expensive dies. No metal spinning operations are needed nor stretch forming. These operations are costly, particularly for reflectors having a diameter greater than ten feet.
- FIGS. 3a and 3b results from the combined effects of petal overlap, fastener hole positions, the number of petals and the thickness of the petal material.
- the transverse bending or curvilinear shape of the petals may be explained by analogy to the bending of beams.
- This space between beams (or petals) can be made as small as possible by reducing ⁇ , l, and/or b so that there is no abrupt change in the slope of the inner surface from one beam (petal) to the next.
- Reducing ⁇ may be achieved by using a greater number of petals.
- Reducing l may be achieved by reducing the diameter of the antenna or using more petals (increasing n).
- Reducing b will reduce the amount of overlap bu may not be desirable because this is what cause the transverse bending. Thus, some trade off among the variables to achieve the best combination is necessary.
- a complete derivation of equation A is given in Appendix A to this specification.
- the maximum stress throughout the petal after assembly should be kept below the endurance limit stress or yield point.
- the maximum stress in the petals is defined by the relationship: ##EQU2## where ⁇ is Poisson's ration, Z o is focal length, E is the elastic modulus of the material and t is the thickness of the petals. A derivation of this equation is given in Appendix B.
- l may be determined from ##EQU4## It is apparent from relationships A and B that the trade off is between ⁇ , l, n, and t, where S max ⁇ t to provide smooth transition from petal-to-petal on the reflector surface.
- the maximum space that will exist between the overlapping edges of adjacent petals may be calculated using equation A.
- equation B the maximum stress may be determined after selecting material E of thickness t. The thickness t is reduced until the maximum stress is substantially below the elastic limit and/or yield point.
- S max By keeping S max less than t the overlap will provide a close and essentially smooth transition from petal-to-petal. This will enhance the conditions necessary for an accurate parabolic surface. If after making the calculation with equation A, the S max may be larger than desirable; if so, it may be desirable to reduce S max by increasing the number of petals, n.
- R 1 , S 1 and R 2 , S 2 and R 3 as shown in FIG. 5. These positions are calculated from the following relationships:
- Outer layer 60 also provides structural support for the reflector, eliminating the need for supporting truss.
- the petals of inner layer 62 are constructed to essentially edgewise abutt one another to eliminate petal-to-petal discontinuities at the reflecting surface which enhances the gain characteristics of the antenna.
- the sheet materials respond non-linearly when deflection, ⁇ , is greater than thickness, t, much more force is required to achive such deflection than for ⁇ less than t.
- the bending of the petal material should be kept within the linear ( ⁇ ⁇ 2t for this fully overlapping configuration) bending range of the material to facilitate field assembly and to avoid support trusses which are necessary to apply greater force yet increase weight and cost. Since the petals of the reflector are to be bent longitudinally as well as transversely, the deflection for a selected number of petals defines t.
- ⁇ increases along the longitudinal axis toward the outer rim of the reflector.
- A the radius of the hole in the center of the dish
- Table III gives the hole positions for the petals in both the outer and inner layers of petals for a 10 foot diameter reflector having a total of 40 petals and a prabolic focal length, Z o , of 48 inches as determined by the above relations.
- Holes S 1 and S 2 are located within ⁇ 0.002 inches and S 3 dimension is located within ⁇ 0.002 inches; holes R 1 and R 2 and dimension R 3 are located within ⁇ 0.002 inches for positions 1-8, within ⁇ 0.005 inches for positions 9-12 and within ⁇ 0.010 for positions 13-22.
- R 1 , S 1 and R 2 , S 2 holes are 0.187/0.189 inch.
- the fastener hole positions and sizes must be precisely located to achieve paraboloidal shape.
- the petal edges are slightly curved outwardly from the longitudinal axis of the petals, precise hole positions would be required only near the center and the outer rim of the assembled reflector (i.e. near the narrowest and widest portions of each petal, respectively) to achieve the same shape. Precise abutting of the curved petal edges rather than precise intermediate hole locations and sizes establishes the paraboloidal shape after assembly.
- the intermediate fasteners now merely maintain the transverse bending of the petal in the overlap region, those fasteners could be of smaller diameter or the holes therefor could be larger to facilitate assembly.
- the assembler simply bends the petal appropriately so that the petals of the inside layer abutt and the intermediate fasteners are inserted.
- the shape of the slightly curved petal edges are defined by:
- Table IV gives values for the R 3 and S 3 dimensions corresponding to the R 1 , S 1 and R 2 , S 2 hole positions given in Table III for a petal having curved edges for uses in the reflector configuration of FIGS. 6a and 6b.
- Table V gives the same data as Table III for a 40 foot diameter reflector having a total of 80 petals and a focal length, Z o , of 192 inches.
- a rectangular plate is subjected to pure bending by moments that are uniformly distributed along the edges of the plate.
Landscapes
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Aerials With Secondary Devices (AREA)
Abstract
Dish reflectors with high gain antennae comprising a plurality of generally triangular shaped petals joined in edgewise overlapping or abutting relation so as to form a substantially paraboloid configuration. Petal configuration is controlled by fastener holes positioned to bend the petal in a substantially parabolic manner along its longitudinal axis and in a substantially curvilinear manner along its transverse axis.
Description
Low-cost, high-gain antenna reflector designs exist in the prior art. One such design is disclosed in U.S. Pat. No. 3,832,717 issued to the inventor hereof Aug. 27, 1974. That design offered the advantages of low cost, light weight and convenient assembly in the field while providing relatively high gain performance up to approximately 4 GHz. However, that reflector, comprising a plurality of generally triangular petals assembled in slightly overlapping relationship, attained only a "quasi-paraboloid" shape which reduces its gain characteristics above 4 GHz. In order to achieve useable gain at frequencies in the 12 GHz region, a reflector having a conformation more closely approaching a true paraboloid is necessary.
True parabolic antennae typically require substantial truss support structure and are expensive to manufacture. The parabolic reflector of the present invention requires no support truss and, by improving the basic design concept of the above-mentioned U.S. patent, achieves substantially parabolic shape over the entire surface of the reflector without appreciably increasing manufacturing cost, complicating field assembly or increasing shipping weight.
One embodiment of the present invention comprises a plurality of greatly overlapping, generally triangular-shaped petals having precisely sized and positioned holes in the overlap region through which a set of fasteners are inserted to locate one petal relative to the next and to bend adjacent petals elastically to provide curvilinear transverse shape therein. For this embodiment the petals may be interlaced or alternately overlayed. Another embodiment of the present invention comprises a layer of generally triangular shaped petals coupled to a second fully overlapping layer of similar shaped petals, the layers being rigidly held together in substantially parabolic conformation by fasteners inserted through commonly and precisely sized and positioned holes through the petals of both layers. For each embodiment, a rigid, segmented exterior rim formed to receive the outer edges of the assembled petals provides the necessary mechanical structure for mounting and positioning the reflector and for maintaining mechanical integrity over a wide range of environmental conditions.
Before assembly of either configuration reflector, each petal is essentially a flat sheet of light-weight, flexible, relatively thin, electromagnetically reflective material such as aluminum. The ultimate reflector configuration is determined by the precisely positioned fasteners in each petal or, alternatively in the case of the two-layer configuration wherein the inner layer petals edgewise abutt, by the shape of the abutting petal edges. Thus, by controlling the locating of the holes in the petals and the shape of the petal edges, the shape of the reflector is controlled and adjusted as desired.
FIG. 1 is a perspective view of a microwave antenna incorporating a prior art quasi-paraboloid dish reflector.
FIG. 2a is a top view of an eight-petal quasi-paraboloid reflector constructed according to FIG. 1 taken at the intersection of the petals with a plane perpendicular to the focal axis of that reflector prior to assembly.
FIG. 2b is a top view of the eight-petal configuration of FIG. 2a after assembly.
FIG. 3a is a top view of an eight-petal paraboloid reflector constructed according to one embodiment of the present invention having interlaced petals taken at the intersection of the petals with a plane perpendicular to the focal axis of that reflector prior to assembly.
FIG. 3b is a top view of an eight-petal paraboloid reflector constructed according to one embodiment of the present invention having alternately overlayed petals taken at the intersection of the petals with a plane perpendicular to the focal axis of that reflector prior to assembly.
FIG. 3c is a top view of the reflector configuration of FIG. 3 during assembly showing curvilinear transverse petal shape
FIG. 4a is a side view of two cantilever beams attached to the same anchor wall.
FIG. 4b is a side view of the top beam of FIG. 4a in bent configuration.
FIG. 5 is a top view of a petal constructed according to one embodiment of the present invention.
FIG. 6a is a top view of a two-layer, 16 petal paraboloid reflector constructed according to another embodiment of the present invention taken at the intersection of the petals with a plane perpendicular to the focal axis of that reflector prior to assembly.
FIG. 6b is a top view of the reflector configuration of FIG. 6a after assembly.
FIG. 7 is a top view of a petal constructed according to another embodiment of the present invention.
FIG. 8 is a three-dimensional view of a parabola as it rotates about the z-axis.
FIG. 9 is a perspective view of a rectangular plate subjected to uniform bending moments.
In the quasi-parabolic reflector of U.S. Pat. No. 3,832,717, each petal slightly overlapped adjacent petals for conveniently indexing the petals to one another during assembly. The overlap was so small that, after assembly, a small, transverse, petal-to-petal angle resulted (refer to FIGS. 1, 2a and 2b) because the overlapped portion of each petal would simply inelastically bend to the angle of the adjacent petal. No smooth, curved bending occurred along common transverse axes of the adjacent petals.
Referring now to FIGS. 3a and 3c, as the interlaced overlap is increased and the petals are fastened with two fasteners, such as rivets or nuts and bolts, at each fastening position in the overlap region, the petals are forced to bend in the transverse direction as shown. The number of fasteners used at each position is essentially arbitrary taking into consideration petal material and thickness. The transverse direction (i.e. axis) is perpendicular to the longitudinal axis of the petal. If the hole positions are located accurately, the petals will form a substantially parabolic reflector. Thus the surface of a reflector need not be preformed using expensive dies. No metal spinning operations are needed nor stretch forming. These operations are costly, particularly for reflectors having a diameter greater than ten feet. When fasteners are installed in the alternately overlayed petal configuration of FIG. 3b, transverse bending is obtained in essentially the same manner.
The reflector design of FIGS. 3a and 3b results from the combined effects of petal overlap, fastener hole positions, the number of petals and the thickness of the petal material. The transverse bending or curvilinear shape of the petals may be explained by analogy to the bending of beams.
Suppose two cantilever beams are attached to the same wall one above the other as shown in FIG. 4a. The bottom beam is shorter than the top beam. Also suppose b is the ratio of the length of the bottom beam to the length of the top beam. (b is analogous to the amount of overlap of one petal over the adjacent petal.) As the top beam is bent such that the end is bent down by an angle φ as shown in FIG. 4b, a gap or space S, will begin to develop between the top and bottom beams (or petals). The maximum amount of this gap is given by the following relation derived from beam theory. ##EQU1## where l is the length of the top beam
This space between beams (or petals) can be made as small as possible by reducing φ, l, and/or b so that there is no abrupt change in the slope of the inner surface from one beam (petal) to the next. Reducing φ may be achieved by using a greater number of petals. Reducing l may be achieved by reducing the diameter of the antenna or using more petals (increasing n). Reducing b will reduce the amount of overlap bu may not be desirable because this is what cause the transverse bending. Thus, some trade off among the variables to achieve the best combination is necessary. A complete derivation of equation A is given in Appendix A to this specification.
If The local yield point stress of the petal material is exceeded during assembly, the petal will be permanently deformed which is undesirable because any such local yielding would indicate a non-uniform stress and/or bending moment which would cause non-uniformity in the curvature of the reflector surface. The maximum stress throughout the petal after assembly should be kept below the endurance limit stress or yield point. The maximum stress in the petals is defined by the relationship: ##EQU2## where ν is Poisson's ration, Zo is focal length, E is the elastic modulus of the material and t is the thickness of the petals. A derivation of this equation is given in Appendix B.
After selecting the number of sections and overlap b, φ may be determined from ##EQU3## where r is the radial distance to any point on the line Z = r2 /4Zo rotated about the Z axis and Zo is the focal length of the parabolic surface of revolution. The maximum value of r is the radius of the antenna.
l may be determined from ##EQU4## It is apparent from relationships A and B that the trade off is between φ, l, n, and t, where Smax < t to provide smooth transition from petal-to-petal on the reflector surface.
Knowing the radius of the dish, the maximum space that will exist between the overlapping edges of adjacent petals may be calculated using equation A. Using equation B, the maximum stress may be determined after selecting material E of thickness t. The thickness t is reduced until the maximum stress is substantially below the elastic limit and/or yield point. By keeping Smax less than t the overlap will provide a close and essentially smooth transition from petal-to-petal. This will enhance the conditions necessary for an accurate parabolic surface. If after making the calculation with equation A, the Smax may be larger than desirable; if so, it may be desirable to reduce Smax by increasing the number of petals, n.
The maximum transverse deflection or bending of a petal along any transverse axis at its intersection with the longitudinal axis is given by: ##EQU5## where n = the number of petals,
Zo = the focal length of the reflector, and δ < t to preclude permanent deformation of the petals. The derivation of equation (C) is given in Appendix C.
The positions of the holes in the petals are now determining from the following relation. If, for example, the radius of the antenna (9.2 fee) is divided into 23 equally spaced lengths, the distance R to each of those 23 positions on the surface of the parabola from the center can be determined by: ##EQU6## where Z = r2 14 Zo , dZ/dr = r/2Zo and r = projection of R on the r-axis after petal is bent longitudinally.
Thus, for each r an R may be calculated. Referring to FIG. 5, a value of θ is now calculated for each r from the following equation:
θ = (180° r)/nR
the R and S positions of each hole position are labeled as R1, S1 and R2, S2 and R3 as shown in FIG. 5. These positions are calculated from the following relationships:
R.sub.1 = Rcos[θ(1-2b)]-0.7
R.sub.2 = Rcos θ -0.7
R.sub.3 = Rcos[θ(1+2b)]-0.7
S.sub.1 = Rsin [θ(1-2b)]
S.sub.2 = Rsin θ
S.sub.3 = Rsin[θ(1+2b)]
where b is the ratio of the overlap to the width of the petal at the fastening point. The constant 0.7 arises from the presence of a circular hole at the center of the assembled reflector. Table I summarized the precise hole positions for each of 80 petals in the example reflector to achieve curvilinear transverse shape in each of those petals.
TABLE I
__________________________________________________________________________
r R R.sub.1
S.sub.1
R.sub.2
S.sub.2
R.sub.3
S.sub.3
__________________________________________________________________________
1 0.400
0.400 0.010 0.021 0.031
2 0.800
0.800
0.100
0.021
0.099
0.042
0.098
0.063
3 1.200
1.201
0.501
0.031
0.500
0.063
0.498
0.094
4 1.600
1.603
0.902
0.042
0.901
0.084
0.898
0.126
5 2.000
2.006
1.305
0.052
1.303
0.105
1.299
0.157
6 2.400
2.410
1.709
0.063
1.706
0.126
1.702
0.108
7 2.800
2.815
2.114
0.073
2.112
0.147
2.107
0.220
8 3.200
3.223
2.522
0.084
2.519
0.167
2.513
0.251
9 3.600
3.633
2.931
0.094
2.928
0.188
2.922
0.282
10 4.000
4.045
3.343
0.105
3.339
0.209
3.333
0.314
11 4.400
4.459
3.758
0.115
3.754
0.230
3.746
0.345
12 4.800
4.877
4.175
0.126
4.171
0.251
4.162
0.377
13 5.200
5.298
4.596
0.136
4.591
0.272
4.582
0.403
14 5.600
5.722
5.020
0.147
5.014
0.293
5.005
0.489
15 6.000
6.149
5.447
0.157
5.441
0.314
5.421
0.471
16 6.400
6.581
5.879
0.168
5.872
0.335
5.861
0.502
17 6.800
7.816
6.314
0.178
6.307
0.356
6.296
0.534
18 7.200
7.456
6.753
0.188
6.746
0.377
6.734
0.565
19 7.600
7.900
7.197
0.199
7.190
0.398
7.177
0.596
20 8.000
8.348
7.646
0.209
7.638
0.419
7.625
0.628
21 8.400
8.802
8.099
0.220
8.091
0.440
8.077
0.659
22 8.800
9.260
8.557
0.230
8.549
0.461
8.534
0.691
23 9.200
9.724
9.021
0.241
9.012
0.482
8.997
0.722
__________________________________________________________________________
In the configuration of FIGS. 6a and 6b, a second layer of essentially identical petals has been added to effectively fully overlap each of the petals in the configuration of FIGS. 3a and 3b. Outer layer of petals 60 is fastened to inner layers of petals 62 by two fasteners (for example, 65) at each fastening position in the overlap region of adjacent petals. The precisely sized and positioned holes serve to index the petals of inner layer 62 to each other when fastened to the petals of outer layer 60, and to cause transverse bending of each petal in the reflector which essentially eliminates petal-to-petal angles when tightly fastened. Equation (C) derived for the greatly overlapped configuration also describes the transverse bending of the petals in layers 60 and 62.
Since the sheet materials respond non-linearly when deflection, δ, is greater than thickness, t, much more force is required to achive such deflection than for δ less than t. In addition, there is substantial risk of exceeding yield point stress and permanently deforming the material. Therefore, the bending of the petal material should be kept within the linear (δ < 2t for this fully overlapping configuration) bending range of the material to facilitate field assembly and to avoid support trusses which are necessary to apply greater force yet increase weight and cost. Since the petals of the reflector are to be bent longitudinally as well as transversely, the deflection for a selected number of petals defines t. If t is too large the bending moment to attain transverse petal deflection would increase beyond the limits of field assembly without special tools, jigs and skilled labor. Therefore, n should be increased to reduce δ which in turn reduces t to facilitate field assembly. Table II gives the maximum transverse deflection of the petals at 10 inch increments of r according to equation (C) for a 10 foot diameter reflector comprising up to 80 petals.
TABLE II
______________________________________
n = 20 n = 30 n = 40 n = 60 n = 80
______________________________________
r = 20"
0.050 0.022 0.013 0.006 0.003
r = 30"
0.110 0.049 0.028 0.012 0.007
r = 40"
0.190 0.084 0.047 0.021 0.012
r = 50"
0.285 0.127 0.071 0.032 0.018
r = 60"
0.392 0.174 0.098 0.044 0.025
______________________________________
It should be noted also that δ increases along the longitudinal axis toward the outer rim of the reflector. The point at which δ = 2t can be controlled by appropriate selection of the parameters discussed above. For this embodiment of the present invention, this point is at the rim along the longitudinal axis of the petal.
The hole positions are determined by the relations given below:
R.sub.1 = Rcos[θ(1-b)]-A
R.sub.2 = Rcos[θ(1+B)]-A
S.sub.1 = Rsin[θ(1-B)]
S.sub.2 = Rsin[θ(1+B)]
Where
A = the radius of the hole in the center of the dish
B = 0.5, the ratio of petal overlap to petal width
R is determined by equation (D) θ = πr/nR
Referring to FIG. 7, Table III gives the hole positions for the petals in both the outer and inner layers of petals for a 10 foot diameter reflector having a total of 40 petals and a prabolic focal length, Zo, of 48 inches as determined by the above relations.
TABLE III
______________________________________
r R R.sub.1
S.sub.1
R.sub.2
S.sub.2
______________________________________
1 7.500 7.508 3.127
0.294 3.081
0.882
2 10.000 10.018 5.635
0.393 5.574
1.175
3 12.500 12.535 8.151
0.491 8.074
1.469
4 15.000 15.061 10.674
0.589 10.582
1.763
5 17.500 17.596 13.208
0.687 13.101
2.057
6 20.000 20.144 15.753
0.785 15.631
2.351
r R R.sub.1
S.sub.1
R.sub.2
S.sub.2
7 22.500 22.704 18.312
0.883 18.175
2.645
8 25.000 25.280 20.886
0.982 20.733
2.939
9 27.500 27.872 23.476
1.080 23.309
3.232
10 30.000 30.481 26.084
1.178 25.902
3.526
11 32.500 33.111 28.711
1.276 28.514
3.820
12 35.000 35.761 31.359
1.374 31.148
4.114
13 37.500 38.433 34.030
1.472 33.804
4.408
14 40.000 41.129 36.724
1.570 36.484
4.702
15 42.500 43.850 39.443
1.669 39.190
4.996
16 45.000 46.597 42.189
1.767 41.921
5.290
17 47.5000 49.373 44.962
1.865 44.681
5.584
18 50.000 52.176 47.765
1.963 47.469
5.878
19 52.500 55.010 50.597
2.061 50.288
6.172
20 55.000 57.876 53.460
2.159 53.138
6.466
21 57.500 60.773 56.356
2.258 56.021
6.760
22 60.000 63.704 59.286
2.356 58.938
7.054
______________________________________
The material used for this embodiment is 5052 H32 aluminum sheet, having thickness, t = 0.050 inches. Holes S1 and S2 are located within ± 0.002 inches and S3 dimension is located within ± 0.002 inches; holes R1 and R2 and dimension R3 are located within ± 0.002 inches for positions 1-8, within ± 0.005 inches for positions 9-12 and within ± 0.010 for positions 13-22. R1, S1 and R2, S2 holes are 0.187/0.189 inch.
For the fully overlapping configuration, where the abutting petal edges are essentially rectilinear, the fastener hole positions and sizes must be precisely located to achieve paraboloidal shape. However, if the petal edges are slightly curved outwardly from the longitudinal axis of the petals, precise hole positions would be required only near the center and the outer rim of the assembled reflector (i.e. near the narrowest and widest portions of each petal, respectively) to achieve the same shape. Precise abutting of the curved petal edges rather than precise intermediate hole locations and sizes establishes the paraboloidal shape after assembly. Then, since the intermediate fasteners now merely maintain the transverse bending of the petal in the overlap region, those fasteners could be of smaller diameter or the holes therefor could be larger to facilitate assembly. After installation of fasteners at the narrowest and widest portions of the petals, the assembler simply bends the petal appropriately so that the petals of the inside layer abutt and the intermediate fasteners are inserted.
The shape of the slightly curved petal edges are defined by:
R.sub.3 = Rcos [θ (1+2B)] -A
s.sub.3 = rsin ]θ(1+2B)]
where A, B, R and θ are defined as above. Again referring to FIG. 7, Table IV gives values for the R3 and S3 dimensions corresponding to the R1, S1 and R2, S2 hole positions given in Table III for a petal having curved edges for uses in the reflector configuration of FIGS. 6a and 6b.
TABLE IV ______________________________________ R.sub.3 S.sub.3 ______________________________________ 3.040 1.173 5.520 1.564 8.007 1.955 10.502 2.347 13.007 2.738 15.524 3.129 18.055 3.520 R.sub.3 S.sub.3 20.600 3.911 23.163 4.302 25.743 4.694 28.343 5.085 30.964 5.476 33.607 5.867 36.275 6.259 38.968 6.650 41.687 7.042 44.435 7.433 47.211 7.824 50.018 8.216 52.857 8.607 55.728 8.999 58.633 9.390 ______________________________________
Referring again to FIG. 7, Table V gives the same data as Table III for a 40 foot diameter reflector having a total of 80 petals and a focal length, Zo, of 192 inches.
TABLE V
__________________________________________________________________________
r R R.sub.1
S.sub.1
R.sub.2
S.sub.2
R.sub.3
S.sub.3
__________________________________________________________________________
1 30.00
30.03
2.52
0.59
2.48
1.77
2.44
2.35
2 37.50
37.56
10.05
0.74
9.99
2.21
9.94
2.94
3 45.00
45.10
17.59
0.88
17.52
2.65
17.46
3.53
4 52.50
52.66
25.15
1.03
25.07
3.09
25.00
4.12
5 60.00
60.24
32.73
1.18
32.64
3.53
32.56
4.71
6 67.50
67.85
40.33
1.33
40.23
3.97
40.14
5.30
7 75.00
75.47
47.96
1.47
47.84
4.42
47.74
5.88
8 82.50
83.13
55.61
1.62
55.49
4.86
55.38
6.47
9 90.00
90.82
63.30
1.77
63.16
5.30
63.04
7.06
10 97.50
98.54
71.02
1.91
70.87
5.74
70.74
7.65
r R R.sub.1
S.sub.1
R.sub.2
S.sub.2
R.sub.3
S.sub.3
11 105.00
106.29
78.77
2.06
78.61
6.18
78.47
8.24
12 112.50
114.09
86.57
2.21
86.40
6.62
86.25
8.83
13 120.00
121.93
94.40
2.36
94.22
7.06
94.06
9.42
14 127.50
129.81
102.28
2.50
102.09
7.51
101.92
10.00
15 135.00
137.73
110.21
2.65
110.00
7.95
109.82
10.59
16 142.50
145.71
118.18
2.80
117.96
8.39
117.78
11.18
17 150.00
153.73
126.20
2.95
125.98
8.83
125.78
11.77
18 157.50
161.81
134.28
3.09
134.04
9.27
133.84
12.36
19 165.00
169.95
142.41
3.24
142.17
9.71
141.95
12.95
20 172.50
178.14
150.61
3.39
150.35
10.16
150.12
13.54
21 180.00
186.39
158.86
3.53
158.59
10.60
158.35
14.12
22 187.50
194.70
167.17
3.68
166.89
11.04
166.65
14.71
23 195.00
203.08
175.55
3.83
175.26
11.48
175.01
15.30
24 202.50
211.53
183.99
3.98
183.69
11.92
183.43
15.89
25 210.00
220.04
192.50
4.12
192.19
12.36
191.92
16.48
26 217.50
228.63
201.09
4.27
200.77
12.81
200.49
17.07
27 225.00
237.28
209.74
4.42
209.41
13.25
209.12
17.66
28 232.50
246.01
218.47
4.56
218.13
13.69
217.83
18.24
29 240.00
254.82
227.27
4.71
226.93
14.13
226.62
18.83
__________________________________________________________________________
Referring to FIG. 4a, generally, ##EQU7##
Referring to FIG. 9, a rectangular plate is subjected to pure bending by moments that are uniformly distributed along the edges of the plate. In a plate undergoing such pure bending the magnitude of the maximum stresses is given by: ##EQU8## where t = thickness of the plate.
In the particular case where Mx = MY = M: ##EQU9## rx = radius of curvature of the plate in x direction ry = radius of curvature of the plate in y direction
E = elastic modulus
ν = Poisson's ratio
A standard approximation in the binding of plates is: ##EQU10## where ω = ω(x, y) is an equation for the deflection of the plate.
In the case of a parabola: ##EQU11## and therefore: ##EQU12## where Zo = focal length
∴ r.sub.x = r.sub.y = 2Z.sub.o (3)
Combining equations (1) and (2): ##EQU13##
Substituting equation (3) into the above equation: ##EQU14##
This equation would apply for the configuration having greatly overlapping petals. For the configuration having fully overlapping petals, two petal sheets effectively act as one. Substituting 2t for t in equation (4): ##EQU15##
Referring to FIG. 8, for paraboloidal deflection in three dimensions, ##EQU16## where n = number of petals
r = radius of reflector
Zo = focal length of reflector
Claims (8)
1. A reflector for high-gain antenna comprising:
a plurality of generally planar triangular electromagnetically reflective petals having a longitudinal axis and rectilinear major edge shape; and
means connecting the petals in edgewise substantially overlapping relation to form a reflector having a shape of a surface of revolution, each petal taking the form along its longitudinal axis of the line that generates the surface of revolution and generally curvilinear transverse form;
the connecting means including a plurality of paired fasteners coupling the overlapping edges of said petals through holes therein at predetermined locations with respect to the longitudinal axis of the petals which define the conformation of the assembled reflector.
2. A reflector as in claim 1 wherein the petals form a reflector of substantially paraboloid shape and each petal is generally of parabolic form along its longitudinal axis.
3. A reflector as in claim 2 wherein the petals, after connection by said connecting means, have a longitudinal form substantially in accordance with the relation Z = r2 /4Zo where r is the radius of a parabola rotating about the Z-axis of a three-dimensional rectangular coordinate system and Zo is the focal length of the resulting parabolic surface of revolution, and have a transverse shape determined substantially in accordance with the relation. ##EQU17## where δ is the amount of curvilinear deflection from rectilinear transverse conformation and n is the number of petals.
4. A reflector as in claim 1 wherein the plurality of petals are in edgewise interlaced substantially overlapping relation.
5. A reflector as in claim 3 wherein δ is less than the thickness of the petal material.
6. A reflector as in claim 1 wherein:
a first plurality of petals are arranged in edgewise substantially abutting relation; and
the connecting means includes a second plurality of essentially identical petals coupled to the first mentioned plurality of petals by the fasteners to form a second fully overlapping layer of petals;
said second layer of petals being effective for forming the first-mentioned plurality of petals into a reflector having substantially paraboloid shape.
7. A reflector as in claim 6 wherein the major shape of the petals is slightly curved outward from the longitudinal axis thereof.
8. A reflector as in claim 6 wherein each of the second plurality of petals have holes located essentially at the same positions relative to the longitudinal axis thereof as each of the first-mentioned plurality of petals.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US05/537,094 US3971023A (en) | 1974-12-30 | 1974-12-30 | Parabolic reflector assembled from triangular shaped petals |
| CA242,650A CA1031071A (en) | 1974-12-30 | 1975-12-29 | Low cost parabolic reflector |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US05/537,094 US3971023A (en) | 1974-12-30 | 1974-12-30 | Parabolic reflector assembled from triangular shaped petals |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3971023A true US3971023A (en) | 1976-07-20 |
Family
ID=24141184
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US05/537,094 Expired - Lifetime US3971023A (en) | 1974-12-30 | 1974-12-30 | Parabolic reflector assembled from triangular shaped petals |
Country Status (2)
| Country | Link |
|---|---|
| US (1) | US3971023A (en) |
| CA (1) | CA1031071A (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4268835A (en) * | 1980-02-04 | 1981-05-19 | Taggart Robert B | Parabolic reflector |
| US4568945A (en) * | 1984-06-15 | 1986-02-04 | Winegard Company | Satellite dish antenna apparatus |
| US4585317A (en) * | 1981-11-05 | 1986-04-29 | Marvin Hodges | Reflector with attenuating connecting plates |
| US4710777A (en) * | 1985-01-24 | 1987-12-01 | Kaultronics, Inc. | Dish antenna structure |
| US4766443A (en) * | 1984-06-15 | 1988-08-23 | Winegard Company | Satellite dish antenna apparatus |
| US4814784A (en) * | 1985-10-23 | 1989-03-21 | Grumman Aerospace Corporation | Individual self-erecting antenna |
| US4841305A (en) * | 1988-02-01 | 1989-06-20 | Dalsat, Inc. | Method of sectioning an antennae reflector |
| CN105390792A (en) * | 2015-11-16 | 2016-03-09 | 深圳市华讯方舟卫星通信有限公司 | Portable satellite communication rotating parabolic antenna |
| US9331394B2 (en) | 2011-09-21 | 2016-05-03 | Harris Corporation | Reflector systems having stowable rigid panels |
| CN110137694A (en) * | 2019-05-29 | 2019-08-16 | 摩比科技（深圳）有限公司 | A kind of antenna reflector |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3234550A (en) * | 1961-06-12 | 1966-02-08 | Washington Aluminum Company In | Thin skinned parabolic reflector with radial ribs |
| US3235872A (en) * | 1963-03-27 | 1966-02-15 | Gen Electronic Lab Inc | Dish reflector formed of similar arcuately arranged thin skinned sections |
| US3832717A (en) * | 1972-03-03 | 1974-08-27 | R Taggart | Dish reflector for a high gain antenna |
-
1974
- 1974-12-30 US US05/537,094 patent/US3971023A/en not_active Expired - Lifetime
-
1975
- 1975-12-29 CA CA242,650A patent/CA1031071A/en not_active Expired
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3234550A (en) * | 1961-06-12 | 1966-02-08 | Washington Aluminum Company In | Thin skinned parabolic reflector with radial ribs |
| US3235872A (en) * | 1963-03-27 | 1966-02-15 | Gen Electronic Lab Inc | Dish reflector formed of similar arcuately arranged thin skinned sections |
| US3832717A (en) * | 1972-03-03 | 1974-08-27 | R Taggart | Dish reflector for a high gain antenna |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4268835A (en) * | 1980-02-04 | 1981-05-19 | Taggart Robert B | Parabolic reflector |
| US4585317A (en) * | 1981-11-05 | 1986-04-29 | Marvin Hodges | Reflector with attenuating connecting plates |
| US4568945A (en) * | 1984-06-15 | 1986-02-04 | Winegard Company | Satellite dish antenna apparatus |
| US4766443A (en) * | 1984-06-15 | 1988-08-23 | Winegard Company | Satellite dish antenna apparatus |
| US4710777A (en) * | 1985-01-24 | 1987-12-01 | Kaultronics, Inc. | Dish antenna structure |
| US4814784A (en) * | 1985-10-23 | 1989-03-21 | Grumman Aerospace Corporation | Individual self-erecting antenna |
| US4841305A (en) * | 1988-02-01 | 1989-06-20 | Dalsat, Inc. | Method of sectioning an antennae reflector |
| US9331394B2 (en) | 2011-09-21 | 2016-05-03 | Harris Corporation | Reflector systems having stowable rigid panels |
| CN105390792A (en) * | 2015-11-16 | 2016-03-09 | 深圳市华讯方舟卫星通信有限公司 | Portable satellite communication rotating parabolic antenna |
| CN105390792B (en) * | 2015-11-16 | 2018-06-01 | 深圳市华讯方舟卫星通信有限公司 | A kind of portable satellite communications rotary parabolic surface antenna |
| CN110137694A (en) * | 2019-05-29 | 2019-08-16 | 摩比科技（深圳）有限公司 | A kind of antenna reflector |
Also Published As
| Publication number | Publication date |
|---|---|
| CA1031071A (en) | 1978-05-09 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US3971023A (en) | Parabolic reflector assembled from triangular shaped petals | |
| US4513293A (en) | Frequency selective antenna | |
| US8405570B2 (en) | Segmented antenna reflector with shield | |
| US3832717A (en) | Dish reflector for a high gain antenna | |
| US4458251A (en) | Concave reflector for radio antenna use | |
| US3740755A (en) | Microwave antenna with radome | |
| US3982248A (en) | Compliant mesh structure for collapsible reflector | |
| US4484198A (en) | Antenna support system with two dimension flexibility | |
| US4268835A (en) | Parabolic reflector | |
| US2989746A (en) | Scanning antenna system utilizing polarization filters | |
| US4783664A (en) | Shaped offset-fed dual reflector antenna | |
| US3122745A (en) | Reflection antenna employing multiple director elements and multiple reflection of energy to effect increased gain | |
| JPH0160962B2 (en) | ||
| JPS6232844B2 (en) | ||
| JP2002353723A (en) | Parabolic antenna with radome | |
| US3569975A (en) | Phase pattern correction for transmitter having a radome | |
| JPS6177404A (en) | Reception antenna for simple satellite broadcast | |
| JP2513996Y2 (en) | Slot array antenna for dual frequency radar | |
| JPS6138261Y2 (en) | ||
| CA1186794A (en) | Dish structure for satellite receiving antenna | |
| USRE26448E (en) | Multiple reflection of energy to effect increased gain | |
| JPS6347061Y2 (en) | ||
| JPS6298805A (en) | Sub-reflection mirror antenna | |
| JPS5951769B2 (en) | Low sidelobe antenna device | |
| JPH047123B2 (en) |